AD Amdt-39-17398
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Pilatus | AIRCRAFT LTD | Airworthiness Directives; PILATUS AIRCRAFT LTD. Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; PILATUS AIRCRAFT LTD. Airplanes |
Unsafe Condition
Failure of the pitch trim actuator and pitch trim actuator components could lead to an unsafe flying configuration.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Rescind AD 2008-07-11, Amendment 39-15452, which mandated new life limits for the pitch trim actuator and pitch trim actuator attachment parts.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 30 days of the effective date (April 15, 2013).
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
PILATUS AIRCRAFT LTD. Models PC-12, PC-12/45, and PC-12/47 airplanes, all serial numbers, certificated in any category.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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